Magnanimous
发表于 2025-3-21 17:58:03
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恭维
发表于 2025-3-21 22:03:30
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Guileless
发表于 2025-3-22 04:21:43
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结合
发表于 2025-3-22 05:13:13
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AWL
发表于 2025-3-22 09:47:52
Incidence and Deviation,xit flow angles. We assumed that the flow is fully congruent with the blade profile. This assumption implies that the inlet and exit flow angles coincide with the camber angles at the leading and trailing edges.
CLASH
发表于 2025-3-22 12:55:23
Blade Design,The blade geometry is adjusted to the stage velocity diagram which is designed for specific turbine or compressor flow applications. Simple blade design methods are available in the open literature (see References).
CLASH
发表于 2025-3-22 20:53:32
Radial Equilibrium,s, ф, λ, r, α. and β.. Assuming an axisymmetric flow with constant meridional velocity and total pressure distributions, we arrived at free vortex flow as a simple radial equilibrium condition with .. .. In practice, from an aerodynamics design point of view, a constant meridional velocity component
cathartic
发表于 2025-3-22 23:18:12
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热情的我
发表于 2025-3-23 03:12:19
Generic Modeling of Turbomachinery Components and Systems,t of several . that we call . (, , , ). Each component is an autonomous entity with a defined function within the system. Inlet nozzles, exit diffusers, combustion chambers, compressors, and turbines are a few component examples. A component may consist of several ..
小步舞
发表于 2025-3-23 08:46:46
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